A control apparatus with an interlock function for each satellite function test is provided to prevent function tests which give a serious impact on a satellite and ground supporting equipment from being performed simultaneously. A control apparatus(200) with an interlock function includes first to fifth relays. The first relay connects a first DC power of ground supporting equipment(100) to a main bus(310) of a satellite(300) through a predetermined diode. The second relay connects the first DC power directly to the main bus of the satellite. The third relay connects a battery(320) of the satellite to the main bus of the satellite. The fourth relay connects a second DC power of the ground supporting equipment to the battery of the satellite. The fifth relay connects a DC electric load of the ground supporting equipment to the battery of the satellite. Therefore, the control apparatus controls the connection between the ground supporting equipment and the satellite.
申请公布号
KR100791322(B1)
申请公布日期
2008.01.04
申请号
KR20060130683
申请日期
2006.12.20
申请人
KOREA AEROSPACE RESEARCH INSTITUTE
发明人
PARK, BYEONG HA;CHOI, JONG YEOUN;KWON, JAE WOOK;YOUN, YOUNG SU;CHO, SEUNG WON